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1. 发明申请

US20150053826A1 VERTICAL TAKE-OFF AND LANDING AIRCRAFT 有权
标题翻译：垂直起落架和飞机
公开(公告)号：US20150053826A1
公开(公告)日：2015-02-26
申请号：US14384053
申请日：2013-03-12
申请人： IHI Corporation
发明人： Masayoshi Tsunekawa , Tetsuya Tamura
IPC分类号： B64C29/00 , B64D31/04
CPC分类号： B64C29/00 , B64C27/20 , B64C27/28 , B64C29/0033 , B64C39/026 , B64D31/04 , B64D35/04
摘要： There is provided a vertical take-off and landing aircraft including: a propulsion mechanism for generating lift and thrust; a power supply unit (e.g. an engine as a power source) for supplying power to the propulsion mechanism; a main frame for supporting the engine, a seat, and a landing undercarriage; a sub-frame for supporting the propulsion mechanism; a frame coupling unit for rotatably coupling the main frame and the sub-frame; and a control stick connected to the sub-frame, so that an occupant sitting on a seat operates a control stick thereby to move the sub-frame relative to the main frame so as to change the orientation of the propulsion mechanism.
摘要翻译：提供了一种垂直起降飞机，包括：用于产生升力和推力的推进机构; 用于向推进机构供电的供电单元（例如作为动力源的发动机）; 用于支撑发动机，座椅和着陆底盘的主框架; 用于支撑推进机构的子框架; 框架联接单元，用于可旋转地联接主框架和子框架; 以及连接到子框架的控制杆，使得坐在座椅上的乘员操作控制杆，从而相对于主框架移动副框架，以便改变推进机构的取向。

2. 发明授权

US09994312B2 Vertical take-off and landing aircraft 有权
公开(公告)号：US09994312B2
公开(公告)日：2018-06-12
申请号：US14886481
申请日：2015-10-19
申请人： IHI CORPORATION
发明人： Masayoshi Tsunekawa , Tetsuya Tamura
IPC分类号： B64C29/00 , B64C3/38 , B64C27/00 , B64C9/24 , B64C11/00
CPC分类号： B64C29/0033 , B64C3/385 , B64C9/24 , B64C11/001 , B64C27/006
摘要： A vertical take-off and landing aircraft includes a propulsion mechanism that generates lift and thrust, a main frame that supports seating and a landing undercarriage, a sub-frame which supports the propulsion mechanism and is arranged so as to be swingable back and forth relative to the main frame, a motive power supply unit supported by the main frame and supplying motive power to the propulsion mechanism, a control stick connected to the sub-frame, and a main wing arranged on the propulsion mechanism, wherein the main wing is formed to be retracted to a position not interfering with an air flow of the propulsion mechanism in a normal time and to be movable to a position where lift is generated when thrust is lost. Gliding is made possible even if thrust is lost while increasing in size of a fuselage is avoided.

3. 发明授权

US09950789B2 Vertical take-off and landing aircraft 有权
公开(公告)号：US09950789B2
公开(公告)日：2018-04-24
申请号：US14669811
申请日：2015-03-26
申请人： IHI Corporation
发明人： Masayoshi Tsunekawa , Tetsuya Tamura
IPC分类号： B64C29/00 , B64C27/20 , B64C27/52 , B64C39/02 , B64C11/00
CPC分类号： B64C29/0033 , B64C11/001 , B64C27/20 , B64C27/52 , B64C39/026
摘要： A vertical take-off and landing aircraft including a propulsion mechanism that generates lift and thrust, a main frame that supports seating and a landing undercarriage, a subframe which supports the propulsion mechanism and which is arranged so as to be swingable back and forth relative to the main frame, motive power supply means supported by the main frame and supplying motive power to the propulsion mechanism, and a control stick connected to the subframe in which the propulsion mechanism includes a pair of ducted fans arranged on a left side and a right side, respectively, of the main frame, swing shafts arranged in the ducted fans, and extending in a horizontal direction, and control vanes connected to the swing shafts, and swinging the control vane enables the subframe to move relative to the main frame. Maneuverability can be improved with addition of control mechanisms restrained.

4. 发明授权

US09963227B2 Vertical take-off and landing aircraft 有权
公开(公告)号：US09963227B2
公开(公告)日：2018-05-08
申请号：US14384053
申请日：2013-03-12
申请人： IHI Corporation
发明人： Masayoshi Tsunekawa , Tetsuya Tamura
IPC分类号： B64C29/00 , B64C27/20 , B64D35/04 , B64D31/04 , B64C27/28 , B64C39/02
CPC分类号： B64C29/00 , B64C27/20 , B64C27/28 , B64C29/0033 , B64C39/026 , B64D31/04 , B64D35/04
摘要： There is provided a vertical take-off and landing aircraft including: a propulsion mechanism for generating lift and thrust; a power supply unit (e.g. an engine as a power source) for supplying power to the propulsion mechanism; a main frame for supporting the engine, a seat, and a landing undercarriage; a sub-frame for supporting the propulsion mechanism; a frame coupling unit for rotatably coupling the main frame and the sub-frame; and a control stick connected to the sub-frame, so that an occupant sitting on a seat operates a control stick thereby to move the sub-frame relative to the main frame so as to change the orientation of the propulsion mechanism.

5. 发明授权

US09561850B2 Vertical take-off and landing aircraft 有权
标题翻译：垂直起降飞机
公开(公告)号：US09561850B2
公开(公告)日：2017-02-07
申请号：US14142403
申请日：2013-12-27
申请人： IHI CORPORATION
发明人： Masayoshi Tsunekawa , Tetsuya Tamura
IPC分类号： B64C29/00 , B64C27/20 , B64C27/52
CPC分类号： B64C29/0033 , B64C27/20 , B64C27/52
摘要： A vertical take-off and landing aircraft includes a propulsion mechanism having a fan for generating lift and thrust, an engine for supplying motive power to the propulsion mechanism, a frame coupling the propulsion mechanism and the engine, seating connected to and suspended from the frame so as to be swingable back and forth relative to the frame, a control stick connected to the frame, and a landing undercarriage connected to the seating, wherein the propulsion mechanism is connected to the frame such that the drive shaft of the fan is directed vertically during landing, and the frame is moved relative to the seating by manipulating the control stick, to change the orientation of the propulsion mechanism. The thrust can be controlled with simple configuration, and take-off and landing can be performed safely even in a small space surrounded by obstacles.
摘要翻译：垂直起降飞机包括具有用于产生升力和推力的风扇的推进机构，用于向推进机构提供动力的发动机，联接推进机构和发动机的框架，连接到框架并悬挂在框架以相对于所述框架来回摆动，连接到所述框架的控制杆和连接到所述座部的着陆底架，其中所述推进机构连接到所述框架，使得所述风扇的驱动轴垂直定向在着陆期间，并且通过操纵控制杆相对于座椅移动框架，以改变推进机构的取向。推力可以通过简单的结构进行控制，即使在被障碍物包围的小空间内也可以安全起飞和着陆。

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